Boundary Conditions for Inhomogeneous Combustion Simulation in Solid Rocket Motors

AIAA JOURNAL(2023)

引用 1|浏览1
暂无评分
摘要
No AccessTechnical NotesBoundary Conditions for Inhomogeneous Combustion Simulation in Solid Rocket MotorsAndrea Di Mascio, Emanuele Martelli, Matteo Bernardini, Fulvio Stella and Agostino NeriAndrea Di Mascio https://orcid.org/0000-0002-9772-3138University of L’Aquila, 67100 L’Aquila, Italy*Full Professor, Department of Industrial and Information Engineering and Economics, Piazzale Ernesto Pontieri 1, Monteluco di RoioMonteluco di Roio, 67100 L'Aquila, Italy; (Corresponding Author).Search for more papers by this author, Emanuele MartelliUniversity of Campania “L. Vanvitelli,” 81100 Caserta, Italy†Associate Professor, Department of Engineering, Via Roma 29—81031 Aversa (CE), Italy.Search for more papers by this author, Matteo Bernardini https://orcid.org/0000-0001-5975-3734University of Rome “Sapienza,” 00184 Rome, Italy‡Associate Professor, Department of Mechanical and Aerospace Engineering, Via Eudossiana 18, 00184 Roma, Italy.Search for more papers by this author, Fulvio StellaUniversity of Rome “Sapienza,” 00184 Rome, Italy§Full Professor, Department of Mechanical and Aerospace Engineering, Via Eudossiana 18, 00184 Roma, Italy.Search for more papers by this author and Agostino NeriEuropean Space Agency, 00044 Frascati, Italy¶Senior Aerospace Principal Engineer, Program Manager of ESA Technical Assistance to Italian PNRR STS.Search for more papers by this authorPublished Online:16 Mar 2023https://doi.org/10.2514/1.J062554SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Fabignon Y., Dupays J., Avalon G., Vuillot F., Lupoglazoff N., Casalis G. and Prevost M., “Instabilities and Pressure Oscillations in Solid Rocket Motors,” Aerospace Science and Technology, Vol. 7, No. 3, 2003, pp. 191–200. https://doi.org/10.1016/S1270-9638(02)01194-X CrossrefGoogle Scholar[2] Flandro G. and Jacobs H., “Vortex Generated Sound in Cavities,” Aeroacoustics Conference, AIAA Paper 1973-1014, 1973. LinkGoogle Scholar[3] Balachandar S., Buckmaster J. and Short M., “The Generation of Axial Vorticity in Solid-Propellant Rocket-Motor Flows,” Journal of Fluid Mechanics, Vol. 429, Feb. 2001, pp. 283–305. https://doi.org/10.1017/S0022112000002688 CrossrefGoogle Scholar[4] Apte S. and Yang V., “A Large-Eddy Simulation Study of Transition and Flow Instability in a Porous-Walled Chamber with Mass Injection,” Journal of Fluid Mechanics, Vol. 477, Feb. 2003, pp. 215–225. https://doi.org/10.1017/S0022112002002987 CrossrefGoogle Scholar[5] Saad T. and Majdalani J., “1On the Lagrangian Optimization of Wall-Injected Flows: From the Hart–McClure Potential to the Taylor–Culick Rotational Motion,” Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, Vol. 466, No. 2114, 2010, pp. 331–362. https://doi.org/10.1098/rspa.2009.0326 CrossrefGoogle Scholar[6] Venugopal P., Moser R. and Najjar F., “Direct Numerical Simulation of Turbulence in Injection-Driven Plane Channel Flows,” Physics of Fluids, Vol. 20, No. 10, 2008, Paper 105103. https://doi.org/10.1063/1.2963137 Google Scholar[7] Wasistho B. and Moser R., “Simulation Strategy of Turbulent Internal Flow in Solid Rocket Motor,” Journal of Propulsion and Power, Vol. 21, No. 2, 2005, pp. 251–263. https://doi.org/10.2514/1.7760 LinkGoogle Scholar[8] Stella F. and Paglia F., “Pressure Oscillations in Solid Rocket Motors: Numerical Study,” Aerospace Science and Technology, Vol. 15, No. 1, 2011, pp. 53–59. CrossrefGoogle Scholar[9] Lupoglazoff N. and Vuillot F., “Comparison between Firing Tests and Numerical Simulation of Vortex Shedding in a 2-D Test Solid Motor,” 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, AIAA Paper 1993-3066, 1993. https://doi.org/10.2514/6.1993-3066 LinkGoogle Scholar[10] Bernardini M., Cimini M., Stella F., Cavallini E., Di Mascio A., Neri A. and Martelli E., “Large-Eddy Simulation of Vortex Shedding and Pressure Oscillations in Solid Rocket Motors,” AIAA Journal, Vol. 58, No. 12, 2020, pp. 5191–5201. LinkGoogle Scholar[11] Massa L., Jackson T., Buckmaster J. and Najjar F., “Fluctuations Above a Burning Heterogeneous Propellant,” Journal of Fluid Mechanics, Vol. 581, June 2007, pp. 1–32. CrossrefGoogle Scholar[12] Gallier S. and Plaud M., “A Model for Solid Propellant Burning Fluctuations Using Mesoscale Simulations,” 7th European Conference for Aeronautics and Space Sciences (EUCASS), EUCASS Committee, 2017. https://doi.org/10.13009/EUCASS2017-144 Google Scholar[13] Moser R., Rogers M. and Ewing D., “Self-Similarity of Time-Evolving Plane Wakes,” Journal of Fluid Mechanics, Vol. 367, July 1998, pp. 255–289. https://doi.org/10.1017/S0022112098001426 CrossrefGoogle Scholar[14] Boyer G., Casalis G. and Estivalèzes J. L., “Stability and Sensitivity Analysis in a Simplified Solid Rocket Motor Flow,” Journal of Fluid Mechanics, Vol. 722, May 2013, pp. 618–644. https://doi.org/10.1017/jfm.2013.90 CrossrefGoogle Scholar[15] Chedevergne F., Casalis G. and Majdalani J., “Direct Numerical Simulation and Biglobal Stability Investigations of the Gaseous Motion in Solid Rocket Motors,” Journal of Fluid Mechanics, Vol. 706, Sept. 2012, pp. 190–218. https://doi.org/10.1017/jfm.2012.245 CrossrefGoogle Scholar[16] Liu C. and Liu Z., eds., “Advances in DNS/LES,” Proceedings of 1st AFOSR International Conference on DNS/LES, Greyden Press, Columbus, OH, Aug. 1997, pp. 137–147. Google Scholar[17] Di Mascio A. and Zaghi S., “An Immersed Boundary Approach for High Order Weighted Essentially Non-Oscillatory Schemes,” Computers & Fluids, Vol. 222, May 2021, Paper 104931. Google Scholar[18] Werner H. and Wengle H., “Large-Eddy Simulation of Turbulent Flow Over and Around a Cube in a Plate Channel,” Turbulent Shear Flows 8, Springer, Berlin, 1993, pp. 155–168. Google Scholar[19] Jiang G. and Shu C., “Efficient Implementation of Weighted ENO Schemes,” Journal of Computational Physics, Vol. 126, No. 1, 1996, pp. 202–228. CrossrefGoogle Scholar[20] Gerolymos G., Sénéchal D. and Vallet I., “Very-High-Order WENO Schemes,” Journal of Computational Physics, Vol. 228, No. 23, 2009, pp. 8481–8524. CrossrefGoogle Scholar[21] Steger J. and Warming R., “Flux Vector Splitting of the Inviscid Gasdynamic Equations with Application to Finite-Difference Methods,” Journal of Computational Physics, Vol. 40, No. 2, 1981, pp. 263–293. CrossrefGoogle Scholar Previous article FiguresReferencesRelatedDetails What's Popular Volume 61, Number 5May 2023 CrossmarkInformationCopyright © 2023 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsCombustionCombustion ChambersEnergyEnergy ConversionEnergy Forms, Production and ConversionEnergy ProductionFluid DynamicsHeat EnginesHeating, Ventilating, and Air ConditioningMass TransferPropellantPropulsion and PowerRocket EngineRocketryThermophysics and Heat Transfer KeywordsSolid Rocket MotorHeterogeneous Solid PropellantCombustion ChambersCourant Friedrichs Lewy ConditionFlame TemperatureVortex Shedding PhenomenaMass Flow RateFluid DynamicsAcknowledgmentThe European Space Agency supported the work through contract no. 4000120618/17/I/AL.PDF Received17 October 2022Accepted24 February 2023Published online16 March 2023
更多
查看译文
关键词
Solid Rocket Motor,Heterogeneous Solid Propellant,Combustion Chambers,Courant Friedrichs Lewy Condition,Flame Temperature,Vortex Shedding Phenomena,Mass Flow Rate,Fluid Dynamics
AI 理解论文
溯源树
样例
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要